IP Library Granted Patent US 9,080,771
Granted Patent B2
US 9,080,771 · App. 13/509,815 · Granted Jul 14, 2015

Combustion chamber having a ventilated spark plug

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Quick Facts
Patent No.
US 9,080,771
App. No.
13/509,815
Granted
Jul 14, 2015
Kind
B2
Abstract

A combustion chamber of a gas turbine engine including a wall, a well secured to the wall, the well forming a recess for a spark plug leading into the combustion chamber, and a spark-plug guide mounted on the well to be transversally mobile relative to the axis of the well, the spark-plug guide including a cylindrical wall portion for guiding and supporting the spark plug and a seal ring mounted such as to engage slidably with a bearing surface of the well. In the combustion chamber the spark-plug guide includes a cooling chamber having openings for supplying cooling air to the chamber.

Claims (12)

1. A combustion chamber of a gas turbine engine comprising:

a wall;

a well secured to the wall, the well forming a recess for a spark plug leading into the combustion chamber;

a spark-plug guide mounted on the well, the spark-plug guide is transversely mobile relative to an axis of symmetry of the well, the spark-plug guide including a cylindrical guide wall portion for guiding the spark plug, a seal ring mounted to bear slidably on a bearing surface of the well, a cylindrical cooling surface portion disposed between the guide wall portion and the seal ring, and a radial surface portion connecting the guide wall portion and the cooling surface portion,

wherein the spark-plug guide includes a cooling chamber delimited by the cooling surface portion and the radial surface portion, the cooling chamber including openings provided on the cooling surface portion for supplying cooling air to the cooling chamber, the cooling chamber providing cooling by impact on an exterior impact surface of the spark plug housed in the spark-plug guide,

wherein an inner diameter of the cooling surface portion is greater than an inner diameter of the guide wall portion, and

wherein a first end of the cooling surface portion is connected to the radial surface portion and a second end of the cooling surface portion is connected to the seal ring.

2. The combustion chamber as claimed in claim 1 , wherein the cooling chamber is annular, the cooling chamber and the cylindrical guide wall portion being coaxial.

3. The combustion chamber as claimed in claim 1 , wherein the cooling chamber is arranged between the cylindrical guide wall portion and the combustion chamber.

4. The combustion chamber according to claim 1 , wherein the cooling air supply openings of the cooling chamber are oriented perpendicularly to an axis of the cooling surface portion.

5. The combustion chamber as claimed in claim 1 , wherein the cooling air supply openings are inclined relative to an axis of the cooling surface portion.

6. The combustion chamber as claimed in claim 1 , wherein a dish is welded to a raised surface of the well bordering the bearing surface of the well, the dish including an opening through which the cylindrical cooling surface portion passes.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 21, 2012
From: BUNEL, JACQUES MARCEL ARTHUR; DE SOUSA, MARIO CESAR; SEVI, GUILLAUME
To: SNECMA
Reel/Frame 028240/0257 →